US6517658B1 - Fiber-resin composite body for providing electromagnetic shielding, comprising an electrical contact strip, and method for making same - Google Patents
Fiber-resin composite body for providing electromagnetic shielding, comprising an electrical contact strip, and method for making same Download PDFInfo
- Publication number
- US6517658B1 US6517658B1 US09/508,081 US50808100A US6517658B1 US 6517658 B1 US6517658 B1 US 6517658B1 US 50808100 A US50808100 A US 50808100A US 6517658 B1 US6517658 B1 US 6517658B1
- Authority
- US
- United States
- Prior art keywords
- fiber fabric
- resin
- contact strip
- electrically conductive
- conductive fiber
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
- B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
- B29C70/885—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/022—Non-woven fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/024—Woven fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/28—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K9/00—Screening of apparatus or components against electric or magnetic fields
- H05K9/0007—Casings
- H05K9/0015—Gaskets or seals
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K9/00—Screening of apparatus or components against electric or magnetic fields
- H05K9/0073—Shielding materials
- H05K9/0081—Electromagnetic shielding materials, e.g. EMI, RFI shielding
- H05K9/009—Electromagnetic shielding materials, e.g. EMI, RFI shielding comprising electro-conductive fibres, e.g. metal fibres, carbon fibres, metallised textile fibres, electro-conductive mesh, woven, non-woven mat, fleece, cross-linked
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
- B32B2307/202—Conductive
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/20—Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
- B32B2307/212—Electromagnetic interference shielding
Abstract
Description
Claims (6)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL1007018A NL1007018C2 (en) | 1997-09-11 | 1997-09-11 | Fiber-plastic composite body for electromagnetic shielding, provided with an electrical contact strip. |
NL1007018 | 1997-09-11 | ||
PCT/EP1998/005712 WO1999012727A1 (en) | 1997-09-11 | 1998-09-02 | Fibre-resin composite body for providing electromagnetic shielding, comprising an electrical contact strip and method for making same |
Publications (1)
Publication Number | Publication Date |
---|---|
US6517658B1 true US6517658B1 (en) | 2003-02-11 |
Family
ID=19765667
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/508,081 Expired - Fee Related US6517658B1 (en) | 1997-09-11 | 1998-09-02 | Fiber-resin composite body for providing electromagnetic shielding, comprising an electrical contact strip, and method for making same |
Country Status (6)
Country | Link |
---|---|
US (1) | US6517658B1 (en) |
EP (1) | EP1011958B1 (en) |
AU (1) | AU9266998A (en) |
DE (1) | DE69820273T2 (en) |
NL (1) | NL1007018C2 (en) |
WO (1) | WO1999012727A1 (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020180104A1 (en) * | 2001-03-29 | 2002-12-05 | Takashi Kobayashi | Robot hand member and method of producing the same |
US20080011510A1 (en) * | 2006-07-12 | 2008-01-17 | General Electric Company | Hybrid faceplate having reduced EMI emissions |
US20080248230A1 (en) * | 2005-06-02 | 2008-10-09 | Nv Bekaert Sa | Polymer Emi Housing Comprising Conductive Fibre |
US20090032643A1 (en) * | 2005-10-25 | 2009-02-05 | The Boeing Company | Environmentally stable hybrid fabric system for exterior protection of an aircraft |
JP2009545468A (en) * | 2006-08-01 | 2009-12-24 | エアバス ドイッチュラント ゲゼルシャフト ミット ベシュレンクテル ハフツング | Layup arrangement and structural arrangement and method for manufacturing components for aerospace industry |
US20100206465A1 (en) * | 2009-02-18 | 2010-08-19 | Fossey Jr William H | Method of fabricating conductive composites |
US20130153140A1 (en) * | 2009-12-11 | 2013-06-20 | Airbus Operations, S.L. | Compaction process of a piece of composite materials |
US9248607B2 (en) | 2011-10-06 | 2016-02-02 | Airbus Operations Gmbh | Method for connecting fiber-reinforced intermediate products for producing a structural fiber composite product, such a structural fiber composite product and a method and device for producing an adhesive layer |
CN106572587A (en) * | 2015-10-08 | 2017-04-19 | 富葵精密组件(深圳)有限公司 | Flexible circuit board and manufacturing method thereof |
US10018210B2 (en) * | 2014-12-19 | 2018-07-10 | Airbus Defence and Space GmbH | Component having an integral bond and joining method |
US10183446B2 (en) | 2014-12-19 | 2019-01-22 | Airbus Defence and Space GmbH | Component having an integral bond and a joining method |
US10597638B2 (en) | 2011-06-29 | 2020-03-24 | Biorestorative Therapies, Inc. | Brown fat cell compositions and methods |
CN115284710A (en) * | 2022-07-06 | 2022-11-04 | 中国人民解放军国防科技大学 | Metal particle interlayer fiber reinforced resin matrix composite material and preparation method thereof |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10009678C1 (en) * | 2000-02-29 | 2001-07-19 | Siemens Ag | Heat conducting adhesive joint between two workpieces used in the production of electronic components comprises a layer of heat conducting material having two flat sided surfaces with openings on each surface |
US7208115B2 (en) * | 2003-03-31 | 2007-04-24 | Lockheed Martin Corporation | Method of fabricating a polymer matrix composite electromagnetic shielding structure |
FR3078654B1 (en) * | 2018-03-12 | 2024-04-19 | Airbus Helicopters | METHOD FOR MANUFACTURING A COMPOSITE STRUCTURE PROVIDED WITH AN ELECTRICALLY CONDUCTIVE LAYER AND COMPOSITE STRUCTURE |
Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0014491A1 (en) * | 1979-01-19 | 1980-08-20 | Borsari & Co. | Double walled container protected against ignition and corrosion and method of making same |
EP0022919A2 (en) * | 1979-07-13 | 1981-01-28 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Method for the impregnation of tissues by resin injection |
US4486490A (en) * | 1979-01-29 | 1984-12-04 | Hexcel Corporation | Electrically conductive prepreg materials |
US4554204A (en) * | 1982-11-06 | 1985-11-19 | Inax Corporation | Fiber reinforced resin molded articles for electromagnetic waves and method for production thereof |
US4681718A (en) * | 1984-05-09 | 1987-07-21 | Hughes Aircraft Company | Method of fabricating composite or encapsulated articles |
US4746389A (en) * | 1987-08-04 | 1988-05-24 | United Technologies Corporation | Method for producing a clean, highly conductive surface for mating composite articles |
EP0399944A2 (en) * | 1989-05-24 | 1990-11-28 | United Technologies Corporation | Composite EMI shield having clean, highly conductive surfaces for conductive bonding |
US5250342A (en) * | 1989-05-24 | 1993-10-05 | United Technologies Corporation | Composite EMI shield having clean, highly conductive surfaces for conductive bonding |
US5698316A (en) * | 1996-10-07 | 1997-12-16 | The Boeing Company | Apparatus and methods of providing corrosion resistant conductive path across non conductive joints or gaps |
US5869412A (en) * | 1991-08-22 | 1999-02-09 | Minnesota Mining & Manufacturing Co. | Metal fibermat/polymer composite |
US5939013A (en) * | 1997-08-25 | 1999-08-17 | Florida State University | Process and apparatus for the production of high strength polymer composite structures |
US6398899B1 (en) * | 1997-01-23 | 2002-06-04 | Shoritsu Plastics Ind. Co., Ltd. | Method for manufacture of EMI shielding |
-
1997
- 1997-09-11 NL NL1007018A patent/NL1007018C2/en not_active IP Right Cessation
-
1998
- 1998-09-02 EP EP98945318A patent/EP1011958B1/en not_active Expired - Lifetime
- 1998-09-02 AU AU92669/98A patent/AU9266998A/en not_active Abandoned
- 1998-09-02 US US09/508,081 patent/US6517658B1/en not_active Expired - Fee Related
- 1998-09-02 WO PCT/EP1998/005712 patent/WO1999012727A1/en active IP Right Grant
- 1998-09-02 DE DE69820273T patent/DE69820273T2/en not_active Expired - Fee Related
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0014491A1 (en) * | 1979-01-19 | 1980-08-20 | Borsari & Co. | Double walled container protected against ignition and corrosion and method of making same |
US4486490A (en) * | 1979-01-29 | 1984-12-04 | Hexcel Corporation | Electrically conductive prepreg materials |
EP0022919A2 (en) * | 1979-07-13 | 1981-01-28 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Method for the impregnation of tissues by resin injection |
US4554204A (en) * | 1982-11-06 | 1985-11-19 | Inax Corporation | Fiber reinforced resin molded articles for electromagnetic waves and method for production thereof |
US4681718A (en) * | 1984-05-09 | 1987-07-21 | Hughes Aircraft Company | Method of fabricating composite or encapsulated articles |
US4746389A (en) * | 1987-08-04 | 1988-05-24 | United Technologies Corporation | Method for producing a clean, highly conductive surface for mating composite articles |
EP0399944A2 (en) * | 1989-05-24 | 1990-11-28 | United Technologies Corporation | Composite EMI shield having clean, highly conductive surfaces for conductive bonding |
US5250342A (en) * | 1989-05-24 | 1993-10-05 | United Technologies Corporation | Composite EMI shield having clean, highly conductive surfaces for conductive bonding |
US5869412A (en) * | 1991-08-22 | 1999-02-09 | Minnesota Mining & Manufacturing Co. | Metal fibermat/polymer composite |
US5698316A (en) * | 1996-10-07 | 1997-12-16 | The Boeing Company | Apparatus and methods of providing corrosion resistant conductive path across non conductive joints or gaps |
US6398899B1 (en) * | 1997-01-23 | 2002-06-04 | Shoritsu Plastics Ind. Co., Ltd. | Method for manufacture of EMI shielding |
US5939013A (en) * | 1997-08-25 | 1999-08-17 | Florida State University | Process and apparatus for the production of high strength polymer composite structures |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7833455B2 (en) | 2001-03-29 | 2010-11-16 | Nippon Oil Corporation | Robot hand member and method of producing the same |
US20050269826A1 (en) * | 2001-03-29 | 2005-12-08 | Nippon Mitsubishi Oil Corporation | Robot hand member and method of producing the same |
US20020180104A1 (en) * | 2001-03-29 | 2002-12-05 | Takashi Kobayashi | Robot hand member and method of producing the same |
US20080248230A1 (en) * | 2005-06-02 | 2008-10-09 | Nv Bekaert Sa | Polymer Emi Housing Comprising Conductive Fibre |
US8276850B2 (en) * | 2005-10-25 | 2012-10-02 | The Boeing Company | Environmentally stable hybrid fabric system for exterior protection of an aircraft |
US8524620B2 (en) | 2005-10-25 | 2013-09-03 | The Boeing Company | Environmentally stable hybrid fabric system for exterior protection of an aircraft |
US20090032643A1 (en) * | 2005-10-25 | 2009-02-05 | The Boeing Company | Environmentally stable hybrid fabric system for exterior protection of an aircraft |
US20090039199A1 (en) * | 2005-10-25 | 2009-02-12 | The Boeing Company | Environmentally stable hybrid fabric system for exterior protection of an aircraft |
US20080011510A1 (en) * | 2006-07-12 | 2008-01-17 | General Electric Company | Hybrid faceplate having reduced EMI emissions |
JP2009545468A (en) * | 2006-08-01 | 2009-12-24 | エアバス ドイッチュラント ゲゼルシャフト ミット ベシュレンクテル ハフツング | Layup arrangement and structural arrangement and method for manufacturing components for aerospace industry |
US8709188B2 (en) | 2006-08-01 | 2014-04-29 | Airbus Operations Gmbh | Lay-up arrangement and structural arrangement and method for producing a component for aerospace |
US8025752B2 (en) * | 2009-02-18 | 2011-09-27 | Raytheon Company | Method of fabricating conductive composites |
US20100206465A1 (en) * | 2009-02-18 | 2010-08-19 | Fossey Jr William H | Method of fabricating conductive composites |
US20130153140A1 (en) * | 2009-12-11 | 2013-06-20 | Airbus Operations, S.L. | Compaction process of a piece of composite materials |
US8932427B2 (en) * | 2009-12-11 | 2015-01-13 | Airbus Operations, S.L. | Compaction process of a piece of composite materials |
US10597638B2 (en) | 2011-06-29 | 2020-03-24 | Biorestorative Therapies, Inc. | Brown fat cell compositions and methods |
US11851682B2 (en) | 2011-06-29 | 2023-12-26 | Biorestorative Therapies, Inc. | Brown fat cell compositions and methods |
US9248607B2 (en) | 2011-10-06 | 2016-02-02 | Airbus Operations Gmbh | Method for connecting fiber-reinforced intermediate products for producing a structural fiber composite product, such a structural fiber composite product and a method and device for producing an adhesive layer |
US10018210B2 (en) * | 2014-12-19 | 2018-07-10 | Airbus Defence and Space GmbH | Component having an integral bond and joining method |
US10183446B2 (en) | 2014-12-19 | 2019-01-22 | Airbus Defence and Space GmbH | Component having an integral bond and a joining method |
CN106572587A (en) * | 2015-10-08 | 2017-04-19 | 富葵精密组件(深圳)有限公司 | Flexible circuit board and manufacturing method thereof |
CN106572587B (en) * | 2015-10-08 | 2019-02-19 | 庆鼎精密电子(淮安)有限公司 | Flexible circuit board and preparation method thereof |
CN115284710A (en) * | 2022-07-06 | 2022-11-04 | 中国人民解放军国防科技大学 | Metal particle interlayer fiber reinforced resin matrix composite material and preparation method thereof |
Also Published As
Publication number | Publication date |
---|---|
WO1999012727A1 (en) | 1999-03-18 |
EP1011958B1 (en) | 2003-12-03 |
NL1007018C2 (en) | 1999-03-12 |
DE69820273D1 (en) | 2004-01-15 |
AU9266998A (en) | 1999-03-29 |
DE69820273T2 (en) | 2004-10-14 |
EP1011958A1 (en) | 2000-06-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: HOLLANDSE SIGNAALAPPARATEN B.V., NETHERLANDS Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:WAGEMAN, FRANCISCUS GERHARDUS JOHANNES;KAPPEL, ERIC ANDRE;REEL/FRAME:011729/0855 Effective date: 20000216 |
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AS | Assignment |
Owner name: THALES NEDERLAND B.V., NETHERLANDS Free format text: CHANGE OF NAME;ASSIGNOR:HOLLANDSE SIGNAALAPPARATEN B.V.;REEL/FRAME:012134/0576 Effective date: 20010409 |
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FPAY | Fee payment |
Year of fee payment: 4 |
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REMI | Maintenance fee reminder mailed | ||
LAPS | Lapse for failure to pay maintenance fees | ||
STCH | Information on status: patent discontinuation |
Free format text: PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362 |
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FP | Lapsed due to failure to pay maintenance fee |
Effective date: 20110211 |